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      https://www.riss.kr/link?id=A100026320

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      다국어 초록 (Multilingual Abstract)

      For rarefied gas flow regimes, physical phenomena such as velocity slip and temperature jump occur on the solid body surface. To predict these phenomena accurately, either the Navier-Stokes solver with a slip boundary condition or the direct simulation Monte Carlo method should be used. In the present study, flow simulations of a wedge were conducted in Mach-10 flow of argon gas for several different flow regimes using a two-dimensional Navier-Stokes solver with the Maxwell slip boundary condition. The results of the simulations were compared with those of the direct simulation Monte Carlo method to assess the present method. It was found that the values of the velocity slip and the temperature jump predicted increase as the Knudsen number increases. Also, the results are comparatively reasonable up to the Knudsen number of 0.05.
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      For rarefied gas flow regimes, physical phenomena such as velocity slip and temperature jump occur on the solid body surface. To predict these phenomena accurately, either the Navier-Stokes solver with a slip boundary condition or the direct simulatio...

      For rarefied gas flow regimes, physical phenomena such as velocity slip and temperature jump occur on the solid body surface. To predict these phenomena accurately, either the Navier-Stokes solver with a slip boundary condition or the direct simulation Monte Carlo method should be used. In the present study, flow simulations of a wedge were conducted in Mach-10 flow of argon gas for several different flow regimes using a two-dimensional Navier-Stokes solver with the Maxwell slip boundary condition. The results of the simulations were compared with those of the direct simulation Monte Carlo method to assess the present method. It was found that the values of the velocity slip and the temperature jump predicted increase as the Knudsen number increases. Also, the results are comparatively reasonable up to the Knudsen number of 0.05.

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      참고문헌 (Reference)

      1 Lockerby, D.A., "Velocity boundary condition at solid walls in rarefied gas calculations" 70 : 2004

      2 Maxwell, J.C, "On Stresses in Rarefied Gases Arising from Inequalities of Temperature" 170 : 231-256, 1879

      3 Lofthouse, A.J, "Nonequilibrium Hypersonic Aerothermodynamics Using the Direct Simulation Monte Carlo and Navier-Stokes Models" University of Michigan 2008

      4 Gökçen, T., "Nonequilibrium Effects for Hypersonic Transitional Flows Using Continuum Approach" 1989

      5 Lockerby, D.A., "Geometric and Constitutive Dependence of Maxwell’s Velocity Slip Boundary Condition" 762 (762): 725-730, 2005

      6 Myong, R.S, "Gaseous Slip Model Based on the Langmuir Adsorption Isotherm" 16 (16): 104-117, 2004

      7 Bird, G.A., "Gas Dynamics and the Direct Simulation of Gas Flows" Oxford University Press 1994

      8 Gökçen, T., "Computational Fluid Dynamics Near the Continuum Limit" AIAA 1987

      9 Blazek, J, "Computational Fluid Dynamics : Principles and Applications" Elsevier Science Ltd 2001

      1 Lockerby, D.A., "Velocity boundary condition at solid walls in rarefied gas calculations" 70 : 2004

      2 Maxwell, J.C, "On Stresses in Rarefied Gases Arising from Inequalities of Temperature" 170 : 231-256, 1879

      3 Lofthouse, A.J, "Nonequilibrium Hypersonic Aerothermodynamics Using the Direct Simulation Monte Carlo and Navier-Stokes Models" University of Michigan 2008

      4 Gökçen, T., "Nonequilibrium Effects for Hypersonic Transitional Flows Using Continuum Approach" 1989

      5 Lockerby, D.A., "Geometric and Constitutive Dependence of Maxwell’s Velocity Slip Boundary Condition" 762 (762): 725-730, 2005

      6 Myong, R.S, "Gaseous Slip Model Based on the Langmuir Adsorption Isotherm" 16 (16): 104-117, 2004

      7 Bird, G.A., "Gas Dynamics and the Direct Simulation of Gas Flows" Oxford University Press 1994

      8 Gökçen, T., "Computational Fluid Dynamics Near the Continuum Limit" AIAA 1987

      9 Blazek, J, "Computational Fluid Dynamics : Principles and Applications" Elsevier Science Ltd 2001

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2027 평가예정 재인증평가 신청대상 (재인증)
      2021-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2018-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2015-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2011-01-01 평가 등재 1차 FAIL (등재유지) KCI등재
      2009-01-01 평가 등재학술지 유지 (등재유지) KCI등재
      2006-01-01 평가 등재학술지 선정 (등재후보2차) KCI등재
      2005-06-16 학술지명변경 외국어명 : Jpurnal of Computatuonal Fluids Engineering -> Korean Society of Computatuonal Fluids Engineering KCI등재후보
      2005-01-01 평가 등재후보 1차 PASS (등재후보1차) KCI등재후보
      2004-01-01 평가 등재후보 1차 FAIL (등재후보1차) KCI등재후보
      2002-07-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.2 0.2 0.19
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.16 0.15 0.405 0.05
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